EP3305459B1 - Procédé de soudage laser, procédé de détermination des conditions de soudage laser, et système de soudage laser - Google Patents

Procédé de soudage laser, procédé de détermination des conditions de soudage laser, et système de soudage laser Download PDF

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Publication number
EP3305459B1
EP3305459B1 EP16802765.4A EP16802765A EP3305459B1 EP 3305459 B1 EP3305459 B1 EP 3305459B1 EP 16802765 A EP16802765 A EP 16802765A EP 3305459 B1 EP3305459 B1 EP 3305459B1
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EP
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Prior art keywords
welding
laser
laser beam
target
locus
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German (de)
English (en)
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EP3305459A4 (fr
EP3305459A1 (fr
Inventor
Tatsuyuki Nakagawa
Yasushi Mukai
Atsuhiro Kawamoto
Junji Fujiwara
Noriyuki Matsuoka
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Panasonic Intellectual Property Management Co Ltd
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Panasonic Intellectual Property Management Co Ltd
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/08—Devices involving relative movement between laser beam and workpiece
    • B23K26/082—Scanning systems, i.e. devices involving movement of the laser beam relative to the laser head
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/20—Bonding
    • B23K26/21—Bonding by welding
    • B23K26/24—Seam welding
    • B23K26/244—Overlap seam welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
    • B23K26/062—Shaping the laser beam, e.g. by masks or multi-focusing by direct control of the laser beam
    • B23K26/0626—Energy control of the laser beam
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
    • B23K26/064—Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms
    • B23K26/0643—Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms comprising mirrors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/20—Bonding
    • B23K26/21—Bonding by welding
    • B23K26/22—Spot welding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/352—Working by laser beam, e.g. welding, cutting or boring for surface treatment
    • B23K26/354—Working by laser beam, e.g. welding, cutting or boring for surface treatment by melting
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/02—Iron or ferrous alloys
    • B23K2103/04—Steel or steel alloys
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
    • B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
    • B23K26/064—Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms
    • B23K26/0648—Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms comprising lenses
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/08—Devices involving relative movement between laser beam and workpiece
    • B23K26/0869—Devices involving movement of the laser head in at least one axial direction
    • B23K26/0876—Devices involving movement of the laser head in at least one axial direction in at least two axial directions
    • B23K26/0884—Devices involving movement of the laser head in at least one axial direction in at least two axial directions in at least in three axial directions, e.g. manipulators, robots

Definitions

  • the present invention relates to a laser welding method of performing welding by irradiating a welding target with a laser beam and a laser welding system.
  • a laser welding method and a laser welding system reflecting the preamble of present claim 1 and present claim 7 are disclosed by the document JP H10 71480 .
  • PTL 1 discloses a technique of promoting release of gas contained in a molten portion by a stirring effect due to laser passing again through a portion welded once in aluminum material.
  • a welding target is irradiated with a laser beam so as to form a beam spot that moves relatively with respect to the welding target along a locus having a spiral shape rotating around a rotation center moving in a welding direction.
  • the welding target is welded using the laser beam irradiated with. While the welding target is irradiated with the laser beam, the welding target is irradiated with the laser beam based on an interval coefficient which is a value indicating an overlapping degree of the locus having the spiral shape in the welding direction.
  • This method suppresses generation of bubbles and provides a preferable welding state of uniform beads.
  • FIG. 1 is a schematic diagram of laser welding system 1001 in accordance with an exemplary embodiment.
  • Laser welding system 1001 includes laser oscillator 1 which outputs laser beam 23, laser head 2 which is a galvanometer scanner head for applying laser beam 23 to welding target 501, and operation controller 5.
  • Laser head 2 includes galvanometer mirror 3, galvanometer motor 4 and F ⁇ lens 6 to scan laser beam 23.
  • Galvanometer mirror 3 changes a locus of laser beam 23.
  • Galvanometer motor 4 causes galvanometer mirror 3 to rotate.
  • An operation of galvanometer motor 4 is controlled by operation controller 5.
  • F ⁇ lens 6 causes laser beam 23 to form an image on welding target 501.
  • Laser welding system 1001 may further include robot 8 having laser head 2 attached thereto to move laser head 2.
  • Robot 8 moves laser head 2 to a target position such that laser beam 23 is relatively scanned by laser head 2.
  • Laser welding system 1001 illustrated in FIG. 1 irradiates laser beam 23 to a predetermined position.
  • Welding target 501 includes metallic plates 30 and 31 overlapping each other.
  • Laser welding system 1001 irradiates metallic plate 30 with laser beam 23 so as to weld metallic plate 30 with metallic plate 31.
  • FIG. 2 is a schematic diagram of laser welding system 1002 in accordance with the embodiment.
  • Laser welding system 1002 includes laser oscillator 1, laser head 7 which is a welding head for applying laser beam 23 output from laser oscillator 1 to welding target 501, robot 8, and operation controller 9.
  • Laser head 7 causes laser beam 23 to form an image on welding target 501.
  • Laser head 7 is attached to a tip of robot 8.
  • Laser head 7 is moved to a target position, and laser head 7 itself is moved so as to scan laser beam 23.
  • Operation controller 9 controls operations of robot 8 and laser head 7.
  • Laser welding system 1002 illustrated in FIG. 2 irradiates laser beam 23 to a predetermined position.
  • Laser welding system 1002 irradiates metallic plate 30 with laser beam 23 so as to weld metallic plate 30 with metallic plate 31.
  • Laser welding system 1001 (1002) includes laser head 2 (7) which apply laser beam 23 output from laser oscillator 1 to welding target 501, robot 8 to which laser head 2 (7) and which moves laser head 2 (7), and controller 17 which controls operations of laser head 2 (7) and robot 8 for laser welding.
  • Laser welding system 1001 (1002) irradiates welding target 501 spirally with laser beam 23.
  • Controller 17 includes welding-target-information input unit 13 and laser-beam-information input unit 14.
  • Welding target information that is information of welding target 501 is input to welding-target-information input unit 13.
  • Laser beam information that is information of the laser beam is input to laser-beam-information input unit 14.
  • the welding target information is of, for example, the shape or the thickness of a joint or the material of welding target 501.
  • the laser beam information is of, for example, a beam diameter or an interval coefficient of laser beam 23.
  • Controller 17 includes welding-condition determining unit 11 which determines a recommended value of welding conditions. That is, welding-condition determining unit 11 determines one or more of a welding speed, a bead width, and a penetration depth of a welded portion as a recommended value Ha based on the information input to the welding-target-information input unit 13, and determines one or more of a rotational frequency and a laser output as recommended value Hb based on the information input to laser-beam-information input unit 14. Controller 17 further includes parameter-change input unit 15 which changes the recommended value determined by welding-condition determining unit 11, and display 16 which displays thereon the recommended value which are determined by welding-condition determining unit 11.
  • the laser beam information includes information of interval coefficient L indicating an overlapping degree of the spiral locus of the laser beam in the welding direction.
  • Controller 17 which controls the operations and the laser welding of laser welding systems 1001 and 1002 is not necessarily an integrated controller, but may be divided into functional blocks which are separate units, such as an operation controller including welding-condition determining unit 11 which controls the operations of laser head 2 (7) and robot 8, and determines the recommended values of the welding conditions, and condition setting unit 12 which inputs and displays the welding conditions or the like.
  • controller 17 further includes storage unit 10 which previously stores interval coefficient L in an appropriate range and beam diameter ⁇ determined by a device specification as fixed values.
  • Information of the beam quality may be input to laser-beam-information input unit 14 as laser beam information, or may be stored in storage unit 10 as information determined based on the device specification. With such units, even an operator with little experience of laser welding can easily determine welding conditions, and can suppress cost for determining construction conditions (time, materials, labor costs, electricity bills, and the like) only by inputting the welding target information and the laser beam information.
  • a configuration in which plural rotating prisms are arranged in the welding head allows a designated position to be scanned and irradiated with laser beam 23.
  • the laser welding of welding target 501 described below can be performed by, for example, laser welding systems 1001 and 1002 illustrated in FIG. 1 and FIG. 2 .
  • a spin locus is a locus of the laser beam which moves in the welding direction while moving the spot along a circular path by the irradiating laser beam. In other words, the spin locus is a locus of the laser beam which relatively moves to the straight line in the welding direction while rotating.
  • the welding in the linear locus was observed under a first welding condition as a comparative example, and a second welding condition.
  • the first welding condition is keyhole type welding in which the inside of the molten pool is irradiated with laser beam 23.
  • FIG. 3 is a sectional view of a welded portion of welding target 501 in welding direction 24 under the first welding condition.
  • a portion of molten pool 22 is moved by irradiating the inside of molten pool 22 with laser beam 23. Accordingly, such welding corresponds to stirring of the molten pool disclosed in PTL 1.
  • metal vapor 26 is generated from the molten portion of welding target 501 by laser beam 23.
  • the reaction force of the generation of the metal vapor forms keyhole 21 which is a hole surrounded by molten metal in molten pool 22.
  • Laser beam 23 is reflected on keyhole 21 plural times to has an energy absorption rate of metal of welding target 501 increasing as laser beam 23 is confined within keyhole 21, thereby providing a sufficient amount of the metal penetration of welding target 501.
  • molten pool 22 which is a liquid phase
  • laser beam 23 moves to welding direction 24 along the welding line of welding target 501
  • a large amount of metal vapor 26 is generated from keyhole front wall 25 which is a liquid phase indicated by a thick solid line of keyhole 21 in welding direction 24.
  • the second welding condition is keyhole type welding in which unmolten portion 34 (solid phase), which is an outer edge of molten pool 22 and is in front of molten pool 22 in welding direction 24, is irradiated with laser beam 23.
  • FIG. 4 is a sectional view of a welded portion of welding target 501 in welding direction 24 under the second welding condition.
  • a molten layer (liquid phase) of molten pool 22 exists on the front side of laser beam 23 in welding direction 24, which is the direction in which the laser beam proceeds.
  • no molten layer (liquid phase) of molten pool 22 exists on the front side of laser beam 23 in welding direction 24.
  • Unmolten portion 34 of welding target 501 which is an outer edge of molten pool 22 and is in front of molten pool 22 in welding direction 24, is irradiated with laser beam 23.
  • This configuration suppresses the occurrence of metal vapor 26 from keyhole front wall 25 indicated by a thick solid line of keyhole 21, and suppresses the collapse of keyhole rear wall 27 of keyhole 21 indicated by a dotted line, thereby reducing the occurrence of bubbles 28.
  • the keyhole type welding is performed in which the inside of molten pool 22 is irradiated with laser beam 23 at welding speed V which is lower than 3m/min while the laser output is adjusted.
  • the keyhole type welding is performed in which the front side of molten pool 22, which is the outer side of molten pool 22, is irradiated with laser beam 23 at welding speed V which is equal to or higher than 3 m/min while the laser output is adjusted.
  • the second welding condition (refer to FIG. 4 ) is preferable as the welding condition providing a preferable welding state in the welding of the linear locus.
  • laser beam 23 is applied not to the inside of the liquid phase of molten pool 22, but to the position toward unmolten portion 34 of the outer edge of molten pool 22 of welding direction 24.
  • the laser welding is performed by irradiation of laser beam 23 at a power density of the laser of laser beam 23 ranging from 105 to 106 (W/cm 2 ).
  • This configuration suppresses the occurrence of the porosities or pits in resolidified layer 29a of bead 29.
  • the relationship between a laser output and a position irradiated with a laser beam is used.
  • the power density is determined based on a combination of the laser output and the beam diameter.
  • FIG. 5 is a top view of welding target 501 in the laser welding of the spin locus.
  • the inside of molten pool 22 in the liquid phase
  • pits 33 in which tiny holes appear in the appearance of the molten portion may occur in the vicinity of center line LC of the bead illustrated in FIG. 5 .
  • FIGs. 6 to 8 are top views of welding target 501 in a case where the spin locus welding is performed under third to fifth welding conditions, respectively.
  • the moving speed in welding direction 24 is identical to one another under the third to fifth welding conditions illustrated in FIGs. 6 to 8 .
  • the moving velocities of the beam spot to form the spiral shape are different from one another under the conditions.
  • FIGs. 5 to 8 illustrate welding target 501 viewing from the side of emitting laser beam 23 regarding the shape of the spin locus (spiral locus) of laser beam 23 and the bead.
  • the occurrence frequency of pits 33 changes depending on the difference in density of the spiral locus, that is, the difference in the density of the spiral interval which is the interval of the spiral locus.
  • the spin interval is coarse, this is, the spin interval is wide, pits 33 are less likely to occur while, in a case where the spin interval is dense, that is, the spin interval is narrow, pits 33 are likely to occur. Accordingly, as the spin interval becomes denser, pits 33 are more likely to occur.
  • FIG. 5 it was confirmed that pits 33 were likely to occur in the vicinity of center line LC which is the center in width direction 24a perpendicular to welding direction 24 of bead 29.
  • beam spot 23a of laser beam 23 passes to contact the region through which beam spot 23a of laser beam 23 passes once.
  • beam spot 23a of laser beam 23 passes through a region separated from the region through which beam spot 23a of laser beam 23 passes once.
  • the welding is performed by spin locus 36 of laser beam 23 along which relatively moves laser beam 23 in welding direction 24 while spirally emitting laser beam 23, the welding is performed such that the spin interval which is the interval between the spiral shapes of spin locus 36 adjacent to each other in welding direction 24 becomes the spin intervals illustrated in FIGs. 6 to 8 under the third to fifth welding conditions, respectively, and then, welding results were observed.
  • beam spot 23a of laser beam 23 moves along spin locus 36, viewing in direction 124a along width direction 24a of bead 29, beam spot 23a passes firstly through center line LC in direction 124a along width direction 24a of bead 29 (indicated by a solid line), and then, passes secondly through center line LC in a direction 224a along width direction 24a of bead 29 opposite to direction 124a (indicated by a broken line). Beam spot 23a thus passes through center line LC of bead 29 twice.
  • FIG. 6 illustrates the shape of spin locus 36 of beam spot 23a of laser beam 23 and bead 29 viewing from the side of emitting laser beam 23 in a case where the welding is performed under the third welding condition.
  • beam spot 23a of laser beam 23 passes again, secondly though the region (indicated by the solid line) which almost (substantially) overlaps the region (indicated by the broken line) through which beam spot 23a of laser beam 23 firstly passes thorough center line LC of bead 29 extending in welding direction 24.
  • beam spot 23a of laser beam 23 passes through center line LC of bead 29 in the bead width direction, and beam spot 23a of laser beam 23 passes through the inside of molten pool 22 (in the liquid phase) again and forms a wider molten pool 22.
  • This configuration similar to the first welding condition (refer to FIG. 3 ), laser beam 23 generates a large amount of metal vapor 26 from keyhole front wall 25 which is a liquid phase of keyhole 21 in the forward direction of spin locus 36. Metal vapor 26 generates bubbles 28, and as a result, pits 33 are likely to occur.
  • FIG. 7 illustrates the shape of spin locus 36 of beam spot 23a and bead 29 viewing from the side of emitting laser beam 23 in a case where the welding is performed under the fourth welding condition.
  • beam spot 23a of laser beam 23 passes again, secondly, through the region (indicated by the broken line) which slightly contacts the region (indicated by the solid line) through which beam spot 23a of laser beam 23 passes firstly on center line LC of bead 29 in the bead width direction.
  • the bead width W changes. Since the spin interval between the spiral shapes of spin locus 36 is wider than the third condition (refer to FIG. 6 ), bead end 29b of bead 29 in width direction 24a has a slightly wavy shape.
  • This configuration suppresses the occurrence of metal vapor 26 from keyhole front wall 25 indicated by the thick solid line of keyhole 21, suppresses the collapse of keyhole rear wall 27 of keyhole 21, and suppresses the generation of bubbles 28, thereby reducing the occurrence of pits 33.
  • FIG. 8 illustrates the shape of spin locus 36 of bead 29 and bead 29 viewing from the side of emitting laser beam 23 in a case where the welding is performed under the fifth welding condition.
  • beam spot 23a of laser beam 23 passes again, secondly through the region (indicated by the broken line) which is located away from the region (indicated by the solid line) through which beam spot 23a of laser beam 23 passes firstly on center line LC of bead 29 in width direction 24a.
  • the spin interval between the spirals of spin locus 36 is wider than the third and fourth welding conditions (refer to FIG. 6 and FIG. 7 ).
  • the width (spiral size) of welding direction 24 in which the spiral shapes rotate is wider than the third and fourth welding conditions (refer to FIG. 6 and FIG. 7 ). Since the speed of the spirally emitted laser beam 23, which is the speed of movement for forming the spiral shape, thus becomes relatively slow, an amount of heat input is concentrated. Therefore, beam spot 23a of laser beam 23 passes again through the liquid phase in molten pool 22 which is melted due to the passing beam spot 23a of laser beam 23, and therefore, the wide molten pool 22 is formed.
  • the occurrence of pits 33 is smaller than under the third welding condition (refer to FIG. 6 ), but pits 33 are concentrated in a portion with a small width in welding direction 24 in which the spiral shapes rotate in direction 24b, in other words, a portion in which the above-described wide molten pool 22 is formed.
  • FIGs. 9A to 11B illustrate the appearance (upper and lower surfaces) of bead 29 when the welding is actually performed under the third to fifth welding conditions (refer to FIG. 6 to FIG. 8 ).
  • FIGs. 9A, 10A, and 11A illustrate the upper surface of bead 29 under the third, fourth, and fifth welding conditions, respectively.
  • FIGs. 9B, 10B, and 11B illustrate the lower surface of bead 29 under the third, fourth, and the fifth welding conditions, respectively.
  • the upper surface illustrated in FIGs. 9A to 11A is a surface of welding target 501 which is irradiated with laser beam 23 and the lower surface is opposite to the upper surface.
  • welding speed V at which the beams spot moves in welding direction 24 is 1 m/min.
  • Rotation radius r at which laser beam 23 rotates is 1.0 mm such that laser beam 23 with the laser output of 2.5 kW is spirally emitted while moving in welding direction 24 at welding speed V
  • the rotational frequency for forming the spiral shapes of laser beam 23 is adjusted so as to meet each of the third to fifth welding conditions. Since the welding speed V is the same under the third to fifth welding conditions, the amount of the heat output to welding target 501 from laser beam 23 is the same.
  • Rotation radius r is equal to the half of the width of spin locus 36 in width direction 24a on bead 29.
  • FIG. 9A illustrating the appearance (surface) of bead 29 welded under the third welding condition (refer to FIG. 6 ), large pits 33 can be continuously confirmed on center line LC of bead 29.
  • FIG. 10A illustrating the appearance (surface) of bead 29 welded under the fourth welding condition (refer to FIG. 7 ), pits 33 are not confirmed in the vicinity of center line LC of bead 29.
  • FIG. 11A illustrating the appearance (surface) of bead 29 welded under the fifth welding condition (refer to FIG. 8 ), in the vicinity of center line LC across which beam spot 23a on spin locus 36 crosses, the small pits 33 are confirmed in a portion where the width in welding direction 24 in which the spiral rotates in direction 24b, that is, in the vicinity of the solidified point in the vicinity of center line LC which is solidified last.
  • the laser welding method according to the embodiment can be performed by, for example, each of the laser welding systems as illustrated in FIG. 1 and FIG. 2 .
  • welding target 501 including metallic plates 30 and 31 overlapping each other is irradiated with laser beam 23 along spin locus 36 in which beam spot 23a relatively moves in welding direction 24 while metallic plate 30 is spirally irradiated with laser beam 23, thereby welding target 501.
  • welding target 501 is welded while avoiding the irradiation of laser beam 23 to the liquid phase portion which is molten pool 22 as much as possible but passing through the solid phase which is unmolten portion 34.
  • beam spot 23a of laser beam 23 passes so as to contact the region through which beam spot 23a of laser beam 23 passes once.
  • beam spot 23a of laser beam 23 passes through a region located away from the region through which beam spot 23a of laser beam 23 passes once.
  • the welding state changes based on the overlapping degree of the spiral locus of laser beam 23 moving in welding direction 24.
  • the overlapping degree of the locus is indicated as interval coefficient L.
  • interval coefficient L for welding speed V and rotation radius r is smaller or larger than the predetermined range, pits 33 are likely to occur.
  • interval coefficient L for welding speed V and rotation radius r is larger than the predetermined range, the heat input changes and uniform bead 29 is not formed. As described above, under welding conditions where interval coefficient L is out of the predetermined designated range, sufficient joint strength cannot be obtained.
  • the spin interval (indicated as interval coefficient L) which is an interval between spiral shapes on spin locus 36 relates to the generation of pits 33.
  • interval coefficient L indicating the overlapping degree of the spiral locus is previously determined, and then, the welding is performed based on interval coefficient L.
  • FIG. 12 illustrates the spiral spin locus 36 of beam spot 23a of laser beam 23.
  • the interval coefficient L which indicates the overlapping degree of the locus of the movement of beam spot 23a of laser beam 23 spirally emitted in welding direction 24 will be described below with reference to FIG. 12 .
  • Beam spot 23a moves relatively with respect to welding target 501 along the locus (spin locus 36) having a spiral shape rotating around the rotation center RC which moves in welding direction 24.
  • Beam spot 23a rotates around the rotation center RC at a rotation frequency F, that is, at a rotation period (1/F) apart from the rotation center RC by rotation radius r.
  • rotation radius r is a predetermined constant value.
  • the interval coefficient L is a value indicating, on spin locus 36, the overlapping degree of the locus of the movement of laser beam 23 spirally emitted, that is, the overlapping degree of portions 36a and 36b of spin locus 36.
  • interval coefficient L is the ratio of width A in welding direction 24 within which beam spot 23a of laser beam 23 rotates around the rotation center RC at the moving velocity 23b having a component in welding direction 24 to width B in welding direction 24 within which beam spot 23a of laser beam 23 rotates around the rotation center RC at the moving velocity 23b having a component of direction 24b opposite to welding direction 24.
  • interval coefficient L is the ratio of width A to width B, and represented by the following formula with beam diameter ⁇ of beam spot 23a, welding speed V at which beam spot 23a moves in welding direction 24, and rotational frequency F of the rotation component of the spiral locus.
  • B W ⁇ ⁇ ⁇ V / 2 ⁇ F
  • Width A is obtained by adding the distance twice rotation radius r to the distance advanced by half cycle time (1/2F) at welding speed
  • V Width B is obtained by subtracting the distance reverse by half cycle time (1/(2 ⁇ F)) at welding speed V by the distance twice rotation radius r. Therefore, widths A and B are obtained by the following formula.
  • A 2 ⁇ r + V / 2 ⁇ F
  • B 2 ⁇ r ⁇ V / 2 ⁇ F
  • Rotation radius r is a rotation radius in width direction 24a of bead 29 as a rotation component of the spiral locus.
  • the relative speed of the beam spot 23a increases in the rotation in welding direction 24 in the spiral.
  • the relative speed of the movement of beam spot 23a is decreased.
  • widths A and B are obtained by the following formulas.
  • A W ⁇ ⁇ + V / 2 ⁇ F
  • B W ⁇ ⁇ ⁇ V / 2 ⁇ F
  • Interval coefficient L which is obtained by the above formulas and is previously determined preferably ranges from 1.5 to 3, and more preferably ranges from 2 to 2.5 to obtain the spin locus under the fourth welding condition (refer to FIG. 7 ).
  • This configuration produces bead 29 having the variation of width direction 24a of bead 29 and the generation of bubbles such as pits 33 suppressed.
  • interval coefficient L When performing the laser welding by using spin locus 36, after changing welding speed V and bead width W, as rotation radius r and the rotational frequency F are calculated by using interval coefficient L, and the values thereof are determined. Even when welding speed V and bead width W are changed, it is possible to perform the welding of spin locus 36 at a certain overlapping degree corresponding to the intended spiral interval coefficient L of laser beam 23, thereby easily adjusting the density of heat input at the welded portion.
  • gap welding in a case where there is a gap in welding target 501 is performed by adjusting the space between spiral shapes of spin locus 36 of laser beam 23 so as to satisfy the range of the optimum values of interval coefficient L. More specifically, in a case where a gap 32 exists between metallic plate 30 (upper plate) and metallic plate 31 (lower plate), the welding condition in which tolerance to gap 32 is increased and welding defects, such as pits 33, are less likely to occur is selected by filling gap 32 with molten pool 22 (melt liquid).
  • remote welding is assumed, and in order to secure a working distance and bead width W, beam diameter ⁇ of beam spot 23a ranges from 0.3 to 1.0 mm.
  • rotation radius r is excessively small, the amount of molten metal is insufficient to fill gap 32.
  • rotation radius r is excessively large, a wide range of metal is melted and thus the laser output becomes insufficient, hardly melting welding target 501 accordingly. Since rotation radius r can be calculated from the relationship between the thickness of the metallic plates and the width of gap 32, rotation radius r can be previously determined by, e.g. experiments.
  • the moving velocity 23b higher than or equal to 3 m/min easily suppresses poor welding, such as pits 33. Accordingly, even in the case of welding on spin locus 36, beam spot 32a is moved preferably at the moving velocity 23b higher than or equal to the above value. In the case of spin locus 36, beam spot 32a passes again through the location where welding target 501 is melted once, and thus it is preferable to move beam spot 23a with the spin interval according to the appropriate interval coefficient L. In a case where the spin interval is small, pits 33 are likely to occur since beam spot 23a passes through molten pool 22 several times.
  • FIG. 13 is a flow chart for determining the laser welding condition of the laser welding method in accordance with the embodiment.
  • welding target information which is information of welding target 501 is input (Step S101).
  • the welding target information includes information of one or more of the material of welding target 501, a joint shape, and a thickness of welding target 501.
  • Laser beam information which is information of laser beam 23 is input (Step S103).
  • the laser beam information includes information of beam diameter ⁇ and interval coefficient L.
  • Recommended values Ha relating to takt time and joint strength are calculated and determined based on the welding target information (Step S102).
  • Recommended values Ha are of one or more of welding speed V, bead width W, and the penetration depth of the welded portion.
  • Recommended values Hb relating to laser behavior is calculated based on the laser beam information and recommended values Ha.
  • Recommended values Hb are of one or more of rotational frequency F and the laser output.
  • Controller 17 displays recommended values Ha and recommended values Hb on display 16 (refer to FIG. 1 and FIG. 2 ) (Step S105).
  • An operator selects whether or not recommended values Ha are changed in accordance with the requirements for welding target 501 (Step S106).
  • controller 17 recalculates and redetermines recommended values Ha (Step S107), and recommended values Hb are recalculated and redetermined in step S104 by using the laser beam information and recommended values Ha redetermined in Step S107, and the resultant is redisplayed in step S105.
  • the values input may be previously stored.
  • Welding speed V determined as recommended value Ha relates to the takt time of machining step.
  • Bead width W is a parameter important to weld joint strength. Therefore, recommended values Ha can be changed in accordance with the embodiment.
  • interval coefficient L in a proper range and beam diameter ⁇ determined by the device specification are previously stored as fixed values in storage unit 10, and may be read out at the time of being used in calculation.
  • a recommended value in the range suitable for the laser oscillator to be used is displayed.
  • the operator can recognize the laser output as recommended value Hb which is recalculated in Step S104 by modifying welding speed V and bead width W in Step S107 so as to obtain intended takt time and joint strength based on the above recommended values.
  • the laser output required for the laser welding of spin locus 36 is calculated by multiplying a correction coefficient by the relationship between welding speed V and the laser output at the time of welding with a linear locus.
  • the correction coefficient represents the effect of dispersion of heat by the laser beam moving along spin locus 36, and is larger than 1 (one).
  • controller 17 does not necessarily display the laser output but does display an error message in Step S105
  • the rotational frequency F determined as recommended value Hb in Step S104 is calculated by the following formula with welding speed V determined as recommended value Ha in Step S102 or Step S107, interval coefficient L in Step S103, bead width W determined as recommended value Ha in Step S102 or Step S107, and beam diameter ⁇ input in Step S103.
  • F V ⁇ L + 1 / L ⁇ 1 / 2 ⁇ W ⁇ ⁇
  • Beam diameter ⁇ is set in Step S103 based on a specification of the laser oscillator, welding speed V is determined as recommended value Ha in Step S102 or Step S107 based on, e.g. the required takt time, and bead width W is determined in accordance with the required joint strength. Therefore, if plural values of interval coefficient L corresponding to plural values of the spin interval indicating the density of the spiral locus on spin locus 36 are previously determined, the rotational frequency F of recommended value Hb can be calculated in Step S104.
  • the spin locus is determined such that beam spot 23a passes through the solid phase portion which is a portion not molten by preventing beam spot 23a from passing through the liquid phase portion which is a portion molten by irradiation of laser beam 23 as much as possible.
  • interval coefficient L indicating the density of the spiral locus of laser beam 23
  • welding target 501 is welded with laser beam 23 relatively moving in welding direction 24 while spirally emitting laser beam 23.
  • welding target 501 is welded by irradiating unmolten portion 34 of welding target 501 with laser beam 23 as much as possible, such that beam spot 23a passes through the solid phase which is unmolten portion 34 by avoiding the irradiation of laser beam 23 to the liquid phase portion which is molten pool 22, for example, beam spot 23a of laser beam 23 passes through again the region (indicated by the broken line) which slightly contacts the region (indicated by the solid line) through which beam spot 23a of laser beam 23 passes firstly on the vicinity of center line LC of bead 29 under the fourth welding condition (refer to FIG. 7 ).
  • Interval coefficient L of the spin locus for irradiating unmolten portion 34 of welding target 501 with laser beam 23 is preferably determined previously by, for example, experiments, the above formulas, and data tables so as to be preferable value and to be within a preferable range.
  • Skilled operators may set welding conditions for obtaining desired welding results in a relatively short time by taking advantage of their experiences of welding phenomenon determined by plural parameters. However, many operators may have little experience of laser welding construction. Operators with little experience spend a lot of time on setting proper laser welding conditions for a robot, an XY table, a laser welding head, and the like.
  • the laser welding method according to the embodiment two or more metallic plates 30 and 31 stacked in a vertical direction are welded by laser beam 23 while suppressing bubbles 28 generated from keyhole rear wall 27 at the time of the laser welding.
  • welding target 501 is welded by irradiating the welding target with laser beam 23 so that laser beam 23 passes through a solid phase portion of metallic plates 30 and 31.
  • the laser output at the time of welding is selected to be equal to or larger than a value sufficient for keyhole type welding.
  • welding speed V of moving in welding direction 24 is preferably equal to or higher than 1 m/min.
  • Welding speed V is preferably selected to be equal to or higher than the speed at which beam spot 23a does not reach the large molten pool 22 as much as possible.
  • the laser welding is performed to two metallic plates 30 and 31 overlapping each other.
  • This laser welding method is also applicable to the laser welding performed to three or more metallic plates overlapping one another.
  • a spiral locus of spin locus 36 may have various shapes, such as a simple spiral shape, a circular shape, a polygonal shape, such as a square or a triangle, and a partially discontinuous arcuate shape as long as spin locus 36 is a continuous locus by scanning and irradiating the welding target with laser beam 23.
  • Interval coefficient L indicates the degree of roughness (overlapping degree) of the spiral locus.
  • the rotation direction of the irradiation with respect to welding direction 24 of beam spot 23a of the beam 23 of spin locus 36 may be clockwise or counterclockwise.
  • welding speed V of laser beam 23, interval coefficient L of laser beam 23, the laser output of laser beam 23 and the like are appropriately set. These parameters may be combined as appropriate by selecting all of or some of these parameters.
  • the laser welding method, the laser welding conditions determining method, and the laser welding system can be applied to the welding of welding target 501 having a lap fillet joint, a butt joint, a T shape joint, an angular joint, an edge joint, and a flare joint.
  • the laser welding method in accordance with the embodiment suppresses the generation of the bubbles and provides uniform bead 29, thus providing a preferable welding state.
  • the laser welding conditions setting method and the laser welding device allow an operator to set information of welding target 501 and information of laser beam 23 so as to determine and display recommended values Ha of the welding conditions, such as the laser output, welding speed V, the welding pattern, the strength of the welded portion, and the penetration of the welded portion, which are suitable for the above setting. Furthermore, even in a case where the operator changes the displayed recommended values Ha, recommended values Hb of the welding condition which are suitable to the changed values can be redetermined and displayed.
  • the system allows welding speed V relating to the takt time and bead width W relating to the joint strength to be changed by an operator, being usable.
  • the system reduces the time and labor for trial and error until the welding conditions are determined, and can reduce burden on the operator regarding the setting of the welding conditions.
  • a laser welding method provides a preferable welding state while suppressing generation of bubbles, and is usefully used as a laser welding method of performing the laser welding by irradiating a welding target with a laser beam.

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  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • Plasma & Fusion (AREA)
  • Mechanical Engineering (AREA)
  • Laser Beam Processing (AREA)

Claims (8)

  1. Procédé de soudage au laser comprenant :
    l'irradiation d'une cible de soudage (501) avec un faisceau laser (23) de manière à former un point de faisceau (23a) qui se déplace relativement par rapport à la cible de soudage (501) le long d'un site (36) ayant une forme de spirale tournant autour d'un centre de rotation (RC) se déplaçant dans une direction de soudage (24) ; et
    le soudage de la cible de soudage (501) en utilisant le faisceau laser (23) avec lequel elle est irradiée, dans lequel
    ladite irradiation de la cible de soudage (501) avec le faisceau laser (23) comprend l'irradiation de la cible de soudage (501) avec le faisceau laser (23) sur la base d'un coefficient d'intervalle (L) qui est une valeur indiquant un degré de chevauchement du site (36) ayant la forme de spirale dans la direction de soudage (24), caractérisé en ce que le coefficient d'intervalle (L) est un rapport d'une première largeur (A) dans la direction de soudage (24), dans laquelle le point de faisceau (23a) tourne autour du centre de rotation (RC) à une vitesse de déplacement ayant une composante dans la direction de soudage, sur une deuxième largeur (B) dans la direction de soudage (24), dans laquelle le point de faisceau (23a) tourne autour du centre de rotation (RC) à une vitesse de déplacement ayant une composante dans une direction (24a) opposée à la direction de soudage.
  2. Procédé de soudage au laser selon la revendication 1, dans lequel le coefficient d'intervalle (L) est le rapport de la première largeur (A) sur la deuxième largeur (B), et se trouve dans une plage allant de 1,5 à 3.
  3. Procédé de soudage au laser selon la revendication 2, dans lequel le coefficient d'intervalle (L) se trouve dans une plage allant de 2 à 2,5.
  4. Procédé de soudage au laser selon la revendication 1, dans lequel
    ledit soudage de la cible de soudage (501) en utilisant le faisceau laser (23) avec lequel elle est irradiée comprend la formation d'un cordon (29) sur la cible de soudage (501) en utilisant le faisceau laser (23) avec lequel elle est irradiée, et
    le coefficient d'intervalle L est représenté par le diamètre de faisceau φ du point de faisceau, la vitesse de soudage V à laquelle le point de faisceau se déplace dans la direction de soudage, la largeur de cordon W, et la fréquence de rotation F d'une composante de rotation du site (36) par une formule suivante : L = A / B ;
    Figure imgb0020
     A = W − ϕ + V / 2 × F ;
    Figure imgb0021
     et B = W − ϕ − V / 2 × F .
    Figure imgb0022
  5. Procédé de soudage au laser selon la revendication 4, dans lequel la fréquence de rotation F est déterminée avec la vitesse de soudage V, le coefficient d'intervalle L, la largeur de cordon W, et le diamètre de faisceau φ du point de faisceau par une formule suivante : F = V × L + 1 / L − 1 / 2 × W − ϕ .
    Figure imgb0023
  6. Procédé de soudage au laser selon la revendication 1, dans lequel
    ledit soudage de la cible de soudage (501) en utilisant le faisceau laser (23) avec lequel elle est irradiée comprend la formation d'un bain de fusion (22) en faisant fondre la cible de soudage (501) avec le faisceau laser (23), et
    ladite irradiation de la cible de soudage (501) avec le faisceau laser (23) comprend l'irradiation, avec le faisceau laser (23), d'une partie non fondue (34) de la cible de soudage (501) située sur un bord extérieur du bain de fusion devant le bain de fusion dans une direction dans laquelle le point de faisceau (23a) se déplace le long du site (36).
  7. Système de soudage au laser (1001 ; 1002) comprenant :
    une tête laser (2 ; 7) qui irradie une cible de soudage (501) avec un faisceau laser (23) ; et
    un dispositif de commande (17) qui commande la tête laser (2 ; 7) et le faisceau laser (23) de sorte que la cible de soudage (501) soit irradiée avec le faisceau laser (23) de manière à former un point de faisceau (23a) qui se déplace relativement par rapport à la cible de soudage (501) le long d'un site (36) ayant une forme de spirale tournant autour d'un centre de rotation (RC) se déplaçant dans la direction de soudage (24), caractérisé en ce que le dispositif de commande (17) comporte :
    une unité d'entrée d'informations de cible de soudage (13) dans laquelle sont entrées des informations de cible de soudage qui sont des informations sur la cible de soudage (501), les informations de cible de soudage comportant des informations d'au moins un parmi un matériau de la cible de soudage (501), une forme d'un joint, et une épaisseur de la cible de soudage (501) ;
    une unité d'entrée d'informations de faisceau laser (14) dans laquelle sont entrées des informations qui sont des informations sur le faisceau laser (23), les informations de faisceau laser comportant des informations d'un coefficient d'intervalle L qui est une valeur indiquant un degré de chevauchement du site (36) ayant la forme de spirale et des informations d'un diamètre de faisceau du faisceau laser (23) ; et
    une unité de détermination des conditions de soudage (11) configurée pour,
    sur la base des informations de cible de soudage, déterminer une ou plusieurs premières valeurs recommandées d'une vitesse de soudage à laquelle le centre de rotation (RC) se déplace dans la direction de soudage, une largeur de cordon W d'un cordon formé dans la cible de soudage (501) avec le faisceau laser (23), et une profondeur de pénétration d'une partie soudée de la cible de soudage (501) avec le faisceau laser (23), et
    sur la base des informations de faisceau laser, déterminer une ou plusieurs deuxièmes valeurs recommandées d'une fréquence de rotation F à laquelle le point de faisceau (23a) tourne autour du centre de rotation (RC) et une sortie de laser du faisceau laser (23) ;
    une unité d'entrée de modification des paramètres (15) qui modifie les premières valeurs recommandées déterminées ; et
    un dispositif d'affichage (16) qui affiche les premières valeurs recommandées déterminées et les deuxièmes valeurs recommandées déterminées,
    dans lequel le coefficient d'intervalle L est un rapport d'une première largeur (A) dans la direction de soudage (24), dans laquelle le point de faisceau (23a) tourne autour du centre de rotation (RC) à une vitesse de déplacement ayant une composante dans la direction de soudage, sur une deuxième largeur (B) dans la direction de soudage (24), dans laquelle le point de faisceau (23a) tourne autour du centre de rotation (RC) à une vitesse de déplacement ayant une composante dans une direction (24b) opposée à la direction de soudage (24).
  8. Système de soudage au laser selon la revendication 7, dans lequel
    l'unité d'entrée d'informations de faisceau laser (14) comporte une unité d'entrée de coefficient d'intervalle à laquelle est entré le coefficient d'intervalle L, et
    l'unité de détermination des conditions de soudage (11) calcule une fréquence de rotation F avec la vitesse de soudage V, le coefficient d'intervalle L, la largeur de cordon W, et un diamètre de faisceau φ du point de faisceau (23a) par la formule suivante : F = V × L + 1 / L − 1 / 2 × W − ϕ .
    Figure imgb0024
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